A320飞机维护手册 AMM HYDRAULIC POWER 液压5(131)

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 9. On the panel 122VU:
 -close the circuit breakers 9XE and 11XE.
 10. After RAT extension:
-push the line key RETURN/TEST STOP on the MCDU.
11. On the ADIRS CDU:
 -set the OFF/NAV/ATT selector switch to OFF position,
 .
 12. On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
 Subtask 29-22-00-869-090
-solenoid 1 of the RAT is energized.
 -the RAT extends.
 NOTE : Do not operate the RAT
____ deployment solenoids for more than 60 seconds. You can operate the solenoids more than once during the test. When the time of operation (solenoids energized) is max. 60 seconds, you must let the solenoids cool for 30 minutes.
On the CAPT PFD:
-
the CAS indication goes back toinitial value,

 -
the test procedure stops.

 B. Retract the RAT (Ref. TASK 29-22-00-869-006).

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 5. Close-up
________ Subtask 29-22-00-860-107
 A. Put the aircraft back to the serviceable condition.
 (1)
 Depressurize the Blue hydraulic system
 (Ref. TASK 29-10-00-864-003).

 (2)
 Do the EIS stop procedure
 (Ref. TASK 31-60-00-860-002)

 (3)
 Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-005).

 (4)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

 

 Subtask 29-22-00-410-076
 B. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the door of the RAT ground control panel 3GE.

 (3)
 Close the access doors 197EB and 195BB.

 (4)
 Remove the safety barriers.

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 Operational Test of the Manual Deployment and the Retraction of the Ram Air Turbine
 1. Reason for the Job
__________________
 To test some components after maintenance
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific 1 SAFETY BARRIERS
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
 Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-22-00-860-007 Installation of the Safety Device of the Ram Air
 Turbine 29-22-00-860-008 Removal of the Safety Device of the Ram Air Turbine 29-22-51-000-010 Removal of the Ram Air Turbine (2GE) 29-22-51-400-010 Installation of the Ram Air Turbine (2GE) 31-60-00-860-001 EIS Start Procedure
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 3. Job Set-up
__________ Subtask 29-22-00-860-108
 A. Aircraft Maintenance Configuration
 (1)
 Put the SAFETY BARRIERS in position adjacent to the location of the RAT (forward of the left main landing-gear door).

 (2)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (3)
 Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).

 (4)
 Make sure that the SAFETY DEVICE - RAT (98D29208246001) is removed from the RAT stowage compartment.

 Subtask 29-22-00-010-082
 B. Open the access door 197EB. Subtask 29-22-00-865-109
 C. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU HYD/RAT/CTL 2801GE D14 106VU CSM/G /EV/MAN/SPLY 6XE B04 121VU HYDRAULIC/RAT/SPLY/EXTN/SOL1 2803GE P33
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 4. Procedure
_________ Subtask 29-22-00-710-067
 A. Operational Test of the Manual Deployment and the Retraction of the RAT
　
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